Author: Hill, Jr. (William A.)
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 102
Book Description
Force, Moment, and Flow-field Characteristics of Two Wing-body-nacelle Combinations at Mach Numbers 2 and 3
Author: Hill, Jr. (William A.)
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 102
Book Description
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 102
Book Description
Force, Moment, and Flow-field Characteristics of Two Wing-body-nacelle Combinations at Mach Numbers 2 and 3
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1714
Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1714
Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Scientific and Technical Aerospace Reports
Investigation, at Inlet Locations, of Fuselage Flow Fields at Transonic and Supersonic Speeds
Author: Lyndell S. King
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 132
Book Description
Wind tunnel tests were conducted to determine the flow distribution about fuselage configurations at transonic and supersonic speeds and at angles of attack up to 20 degrees. The models tested were approximately one-twelfth scale and consisted of a main fuselage forebody member and several attachable components. The components were mounted in several combinations to represent different possible configurations for tactical aircraft. Flow distribution surveys were conducted at two inlet locations ahead of and under the wing to assess the effects of forebody geometry for the conditions indicated. The data indicate the influence of the canopy, nose droop, and fuselage shape on flow angularities in the forward survey plane.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 132
Book Description
Wind tunnel tests were conducted to determine the flow distribution about fuselage configurations at transonic and supersonic speeds and at angles of attack up to 20 degrees. The models tested were approximately one-twelfth scale and consisted of a main fuselage forebody member and several attachable components. The components were mounted in several combinations to represent different possible configurations for tactical aircraft. Flow distribution surveys were conducted at two inlet locations ahead of and under the wing to assess the effects of forebody geometry for the conditions indicated. The data indicate the influence of the canopy, nose droop, and fuselage shape on flow angularities in the forward survey plane.
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1440
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1440
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Determination of Captive Flight Loads and Separation Trajectories of Airborne Stores
Author: Dale E. Knutsen
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 72
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 72
Book Description
NASA Technical Note
Measurements of Flow Properties in the Vicinity of Three Wing-fuselage Combinations at Mach Numbers of 1.61 and 2.01
Author: Harry W. Carlson
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 78
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 78
Book Description